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AEROACOUSTIC DESIGN AND BROADBAND NOISE PREDICTIONS OF A TURBOFAN STAGE WITH SERRATED OUTLET GUIDE VANES

机译:具有锯齿出口导向叶片的涡轮机舞台的空气声学设计和宽带噪声预测

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This work, realized in the framework of the European project TurboNoiseBB, presents the aeroacoustic design of serrated OGVs (Outlet Guide Vanes), including details on their broadband noise and aerodynamic performance. The serrated OGV corresponds to a modified stator from a turbofan model tested at the AneCom facility (Germany) and shared by the Consortium. Leading edge sinusoidal patterns with varying amplitude and wavelength along the span are designed in collaboration with Safran Aircraft Engines. Serrations are adjusted to account for the turbulence characteristics provided by RANS calculations. Optimal parameters are found using simple design rules discussed in the paper. Down selection of serrated OGV designs (patent pending) was performed in accordance with industrial specifications. Broadband noise simulations are performed using a CAA code solving the linearized Euler equations with a synthetic turbulence model. Numerical predictions at approach conditions are compared to available experimental measurements and an analytical Amiet-based model. Predictions on the untreated case show a fairly good agreement by comparison to the PSD measured at the bypass casing, and a PWL reduction around 3-4 dB roughly estimated by the design process is numerically achieved by the present method.
机译:这项工作在欧洲项目TurboroiseBB的框架内实现,呈现出锯齿状OGV(出口导叶片)的气动声学设计,包括宽带噪声和空气动力学性能的细节。锯齿状的OGV对应于在Anecom设施(德国)测试的涡轮机模型的修改定子,并由联盟共享。沿着跨度的具有变化幅度和波长的前缘正弦图案是与Safran飞机发动机合作的。调整锯齿以考虑RAN计算提供的湍流特性。使用本文中讨论的简单设计规则找到了最佳参数。根据工业规范进行锯齿化OGV设计的选择(专利申请)。使用具有用合成湍流模型的CAA码求解线性化欧拉方程的CAA码进行宽带噪声模拟。将接近条件的数值预测与可用的实验测量和基于分析的亚替氏模型进行了比较。通过与在旁路壳体上测量的PSD的比较,对未处理案例的预测显示了相当良好的一致性,并且通过本方法数量地实​​现了由设计过程大致估计的PWL减小约为3-4dB。

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